ATE534574T1 - Querstossverbindung zwischen zwei rumpsektionen sowie verfahren zur herstellung derselben - Google Patents

Querstossverbindung zwischen zwei rumpsektionen sowie verfahren zur herstellung derselben

Info

Publication number
ATE534574T1
ATE534574T1 AT09720770T AT09720770T ATE534574T1 AT E534574 T1 ATE534574 T1 AT E534574T1 AT 09720770 T AT09720770 T AT 09720770T AT 09720770 T AT09720770 T AT 09720770T AT E534574 T1 ATE534574 T1 AT E534574T1
Authority
AT
Austria
Prior art keywords
fuselage sections
transverse butt
wedge
skin
producing
Prior art date
Application number
AT09720770T
Other languages
English (en)
Inventor
Stefan Tacke
Stephan Mischereit
Volker Reye
Original Assignee
Airbus Operations Gmbh
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Application granted granted Critical
Publication of ATE534574T1 publication Critical patent/ATE534574T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B64C1/069—Joining arrangements therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2211/00—Modular constructions of airplanes or helicopters
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Tires In General (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Body Structure For Vehicles (AREA)
AT09720770T 2008-03-10 2009-02-16 Querstossverbindung zwischen zwei rumpsektionen sowie verfahren zur herstellung derselben ATE534574T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102008013365A DE102008013365B4 (de) 2008-03-10 2008-03-10 Querstoßverbindung zwischen zwei Rumpfsektionen
PCT/EP2009/051776 WO2009112327A1 (de) 2008-03-10 2009-02-16 Querstossverbindung zwischen zwei rumpfsektionen

Publications (1)

Publication Number Publication Date
ATE534574T1 true ATE534574T1 (de) 2011-12-15

Family

ID=40606158

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09720770T ATE534574T1 (de) 2008-03-10 2009-02-16 Querstossverbindung zwischen zwei rumpsektionen sowie verfahren zur herstellung derselben

Country Status (7)

Country Link
US (1) US8444090B2 (de)
EP (1) EP2257467B1 (de)
CN (1) CN101959753B (de)
AT (1) ATE534574T1 (de)
DE (1) DE102008013365B4 (de)
RU (1) RU2467919C2 (de)
WO (1) WO2009112327A1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0901640D0 (en) * 2009-02-03 2009-03-11 Airbus Uk Ltd Joint
ES2385906B1 (es) * 2009-09-30 2013-06-17 Airbus Operations, S.L. Disposición de unión circunferencial de elementos estructurales con un elemento de acoplamiento realizado en material compuesto.
ES2396838B1 (es) * 2010-09-13 2014-02-06 Airbus Operations S.L. Disposición de unión de piezas de material compuesto reforzada direccionalmente.
DE102010047561B4 (de) 2010-10-07 2013-07-25 Airbus Operations Gmbh Klemmvorrichtung und Verfahren zur Montage von Stringerkupplungen
DE102011004844A1 (de) * 2011-02-28 2012-08-30 Airbus Operations Gmbh Türrahmenverbund, Rumpfabschnitt sowie Luft- oder Raumfahrzeug
US8870118B2 (en) * 2012-05-07 2014-10-28 The Boeing Company Method and systems for use in assembling a fuselage
US8960606B2 (en) * 2012-10-31 2015-02-24 The Boeing Company Circumference splice for joining shell structures
DE102013102812B4 (de) * 2013-03-19 2017-01-26 Airbus Operations Gmbh Rumpfstruktur für ein Verkehrsmittel, Verkehrsmittel und Verfahren zum Herstellen einer Rumpfstruktur für ein Verkehrsmittel
EP2799220B1 (de) * 2013-04-30 2020-06-17 Airbus Operations S.L. Verbundstruktur für ein Flugzeug und Herstellungsverfahren dafür
DE102016210325B4 (de) 2016-06-10 2021-07-15 Airbus Operations Gmbh Bauteilanordnung zur Ausbildung einer Tragstruktur eines Luft- oder Raumfahrzeugs
DE102017101531B4 (de) 2017-01-26 2024-09-26 Airbus Operations Gmbh Verformbare Distanzmasse und Befestigungsanordnung
CN107477281B (zh) * 2017-09-16 2022-12-27 中国海洋大学 一种海洋纤维增强复合管用双限制连接系统
EP3698955B1 (de) * 2019-02-19 2021-10-27 Muelles Y Ballestas Hispano-Alemanas Projects, S.L. Versteifte platte aus verbundwerkstoff und verfahren zur herstellung dieser platte
US11524762B2 (en) * 2020-02-21 2022-12-13 The Boeing Company Fuselage structure splice
EP4129817A1 (de) 2021-08-06 2023-02-08 Airbus Operations GmbH Verfahren zum verbinden von strukturprofilen
GB2612958B (en) * 2021-11-08 2023-12-20 Airbus Operations Ltd Panel assembly

Family Cites Families (22)

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Publication number Priority date Publication date Assignee Title
US2405643A (en) * 1944-02-07 1946-08-13 Lockheed Aircraft Corp Structural connector
US4113910A (en) * 1977-04-27 1978-09-12 Rockwell International Corporation Composite load coupler for reinforcing composite structural joints
US4892435A (en) * 1989-02-06 1990-01-09 Grumman Aerospace Corporation Interlocking structural members employing transverse locking double interfitting wedge
RU2000248C1 (ru) * 1992-01-17 1993-09-07 КацИ.Л. Отсек ракетоносител
US5518208A (en) * 1993-12-28 1996-05-21 The Boeing Company Optimum aircraft body frame to body skin shear tie installation pattern for body skin/stringer circumferential splices
CN1051520C (zh) * 1996-10-07 2000-04-19 王新云 飞行器的预应力结构及制造方法
JP2000006893A (ja) * 1998-06-23 2000-01-11 Fuji Heavy Ind Ltd 複合材翼構造
EP1081043A1 (de) * 1999-08-23 2001-03-07 British Aerospace Public Limited Company Herstellung und Montage von Strukturen
US6478922B1 (en) * 2000-06-15 2002-11-12 Alliant Techsystems Inc. Method of manufacturing a composite structure using a conformable locating aperture system
WO2002067652A2 (en) * 2001-01-16 2002-09-06 Monsanto Technology Llc Novel mutilple shoot proliferation and regeneration system for plants
US20040035979A1 (en) * 2002-08-23 2004-02-26 Mccoskey William Robert Integrally stiffened axial load carrying skin panels for primary aircraft structure and closed loop manufacturing methods for making the same
US7197852B2 (en) * 2002-09-20 2007-04-03 The Boeing Company Internally stiffened composite panels and methods for their manufacture
FR2863673B1 (fr) * 2003-12-10 2006-03-10 Airbus France Dispositif d'assemblage par rivetage de plusieurs elements et procede d'assemblage de panneaux notamment de fuselage d'aeronef a l'aide dudit dispositif
DE102004001078B8 (de) * 2004-01-05 2013-06-13 Airbus Operations Gmbh Flugzeugrumpf
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
DE102005033992B3 (de) * 2005-07-21 2007-04-19 Airbus Deutschland Gmbh Verfahren zum Verbinden von mindestens zwei Flächengebilden, insbesondere von mindestens zwei Metallblechen für eine Leichtbaustruktur sowie Verbindung und Leichtbaustruktur
GB0525896D0 (en) * 2005-12-20 2006-02-01 Airbus Uk Ltd A joint for use in aircraft construction
FR2915458B1 (fr) * 2007-04-25 2010-01-01 Airbus France Assemblage de panneaux de fuselage d'un avion
US8042315B2 (en) * 2007-09-14 2011-10-25 Spectrum Aeronautical, Llc Reinforced composite panel
DE102007055233A1 (de) * 2007-11-20 2009-05-28 Airbus Deutschland Gmbh Kupplungsvorrichtung zum Zusammenfügen von Rumpfsektionen, Kombination aus einer Kupplungsvorrichtung und zumindest einer Rumpfsektion sowie Verfahren zur Herstellung der Kupplungsvorrichtung
US8038099B2 (en) * 2008-04-30 2011-10-18 The Boeing Company Bonded metal fuselage and method for making the same
ES2390318B1 (es) * 2009-03-10 2013-09-16 Airbus Operations, S.L. Estructura cerrada en material compuesto.

Also Published As

Publication number Publication date
US8444090B2 (en) 2013-05-21
DE102008013365B4 (de) 2011-03-17
RU2467919C2 (ru) 2012-11-27
US20100320322A1 (en) 2010-12-23
DE102008013365A1 (de) 2009-10-01
EP2257467A1 (de) 2010-12-08
EP2257467B1 (de) 2011-11-23
RU2010141521A (ru) 2012-04-20
WO2009112327A1 (de) 2009-09-17
CN101959753A (zh) 2011-01-26
CN101959753B (zh) 2014-07-23

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